Large-Eddy Simulation of a multi-element wing section

Описание к видео Large-Eddy Simulation of a multi-element wing section

LEISA2 test case from AIAA BANC workshops: Mach number=0.178, AoA=6.15°, Reynolds number=1.23e6
The multi-element wing section is modeled with immersed boundary conditions (IBC).
Automatic Cartesian mesh generation and IBC pre-processing are performed by Cassiopée ( https://cassiopee.onera.fr ). The Fast solver ( https://fast.onera.fr ) is used to run the LES simulation with AUSM scheme.

Author: T. Renaud (ONERA)

00:00 Flight conditions
00:20 Density gradient magnitude slice
00:38 Q Criterion
01:02 View from slat
01:12 View from flap

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